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Faculty Profile
To Dr. Shih's Web Page
E-mail address: shih@eng.fsu.edu
236 CEB, (850) 410-6321
Dr. Chiang
Shih, Departmental Chair and Professor of Mechanical Engineering,
received his Ph.D. degree from the Aerospace Engineering Department at
University of Southern California in 1988. He joined the Department of
Mechanical Engineering in August, 1988. Dr. Shih's research interests
are in the areas of unsteady aerodynamics, separated flow control, aeroacoustics,
optical diagnostic techniques and MEMS applications in flow control. He
currently conducts research on the development of micro-diagnostics system
and supersonic jet noise control.
Published Articles
- Lee, G.-B., Shih, C., Tai, Y.-C., Tsao, T., Liu C., Huang, A., and
Ho, C.-M., "Robust Vortex Control of a Delta Wing Using Distributed
MEMS Actuators," Accepted by Journal of Aircraft, to appear, 2000.
- Shih, C., Alvi, F.S., and Washington, D.M., "The Effects of Counterflow
on the Aeroacoustic Properties of a Supersonic Jet," Journal of Aircraft,
Vol. 36, No. 2, pp. 451-457, 1999.
- Gogineni, S., Visbal, M. and Shih, C., "Phase-Resolved PIV Measurements
in a Transitional Plane Wall Jet: A Numerical Comparsion," Experiment
in Fluids, Vol. 27, PP. 126-136,1999.
- Gogineni, S., Shih, C., "An Experimental Investigation of the Unsteady
Structure of a Transitional Plane Wall Jet", Vol. 23, pp. 121-129, 1997
- Shih, C. and Ding, Z., "Trailing-Edge Jet Control of Leading-Edge
Vortices of a Delta Wing," AIAA Journal, Vol. 34, No. 7, pp. 1447-1457,
July 1996.
- Shih, C. and Ding, Z., "Trailing-Edge Jet Control of Leading-Edge
Vortices of a Delta Wing," AIAA Journal, Vol. 34, No. 7, pp. 1447-1457,
July 1996.
- Shih, C., Lourenco, L., and Krothapalli, A., "Investigation of Flow
Past Leading and Trailing Edges of a Pitching-Up Airfoil," AIAA Journal,
Vol. 33, No. 8, pp. 1369-1376, Aug. 1995.
- Shih, C. and Gogineni, S., "Experimental Study of Perturbed Laminar
Wall Jet," AIAA Journal, Technical Note, Vol. 33, No. 3, pp.559-561,
1995.
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Last Update: 8/25/02. For questions, see the contact
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